Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method

A turbine component (56) adapted for use in a hot gas path of a gas turbine having a thermal barrier coating (62) on at least one surface portion thereof, the turbine component further comprising a protective top coating (64) of predetermined thickness, the thickness determined as a function of in-u...

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Hauptverfasser: BRUCE, KEVIN LEON, MEYER, ROBERT CARL, DEBELLIS, LISA, STOWELL, WILLIAM R, SEAL, MICHAEL DAMIAN, CLARE, JAMES H, ARNESS, BRIAN P, SKOOG, ANDREW JAY, MURPHY, JANE ANN, MARKS, PAUL THOMAS, ROWE, RAYMOND GRANT, MCGOVERN, TARA E, ROLING, MATHEW CURTIS
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Sprache:eng ; fre ; ger
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creator BRUCE, KEVIN LEON
MEYER, ROBERT CARL
DEBELLIS, LISA
STOWELL, WILLIAM R
SEAL, MICHAEL DAMIAN
CLARE, JAMES H
ARNESS, BRIAN P
SKOOG, ANDREW JAY
MURPHY, JANE ANN
MARKS, PAUL THOMAS
ROWE, RAYMOND GRANT
MCGOVERN, TARA E
ROLING, MATHEW CURTIS
description A turbine component (56) adapted for use in a hot gas path of a gas turbine having a thermal barrier coating (62) on at least one surface portion thereof, the turbine component further comprising a protective top coating (64) of predetermined thickness, the thickness determined as a function of in-use temperature of the thermal barrier coating.
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MATERIAL</subject><subject>DYES</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>FILLING PASTES</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL</subject><subject>INKS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>MISCELLANEOUS APPLICATIONS OF MATERIALS</subject><subject>MISCELLANEOUS COMPOSITIONS</subject><subject>NATURAL RESINS</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PAINTS</subject><subject>PASTES OR SOLIDS FOR COLOURING OR PRINTING</subject><subject>POLISHES</subject><subject>STEAM ENGINES</subject><subject>SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION</subject><subject>USE 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adapted for use in a hot gas path of a gas turbine having a thermal barrier coating (62) on at least one surface portion thereof, the turbine component further comprising a protective top coating (64) of predetermined thickness, the thickness determined as a function of in-use temperature of the thermal barrier coating.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
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language eng ; fre ; ger
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subjects ADHESIVES
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CHEMICAL PAINT OR INK REMOVERS
CHEMICAL SURFACE TREATMENT
CHEMISTRY
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATIONOR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY IONIMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
COATING COMPOSITIONS, e.g. PAINTS, VARNISHES ORLACQUERS
COATING MATERIAL WITH METALLIC MATERIAL
COATING METALLIC MATERIAL
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
CORRECTING FLUIDS
DIFFUSION TREATMENT OF METALLIC MATERIAL
DYES
ENGINE PLANTS IN GENERAL
FILLING PASTES
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL
INKS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METALLURGY
MISCELLANEOUS APPLICATIONS OF MATERIALS
MISCELLANEOUS COMPOSITIONS
NATURAL RESINS
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PAINTS
PASTES OR SOLIDS FOR COLOURING OR PRINTING
POLISHES
STEAM ENGINES
SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION
USE OF MATERIALS THEREFOR
WEAPONS
WOODSTAINS
title Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method
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